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global shared weld node list 1 expanding memory to 17157824 d 7974569047 global shared weld node list 2 expanding memory to 17157857 d 8246167087 mpp general scratch S t o r a

3052 4 2

用户_25500 2年前

问答求助，这是什么问题呀，几分钟就莫名中断？

global shared weld node list 1 expanding memory to 13620578 d 5408770595 global shared weld node list 2 expanding memory to 13620611 d 5596404347 mpp general scratch S t o r a

3083 2 1

用户_25500 2年前

帖子 ansys workbench mechanical 所有命令

key: Description: Generate supports for the bodies that are part of the build.

4786 4 3

yyddss 12月前

问答用inp文件定义局部坐标各向异性报错怎么解决？

=NO, contact=NO**** PARTS***Part, name=Part-1*Node 1, -0.00999999978, -0.00999999978, 0.0199999996 2, -0.00999999978, 0., 0.0199999996 3, -0.00999999978

2680 3

。_0381 3年前

问答提问：用CEL分析受液体挤压金属的变形时为什么会出现欧拉节点被绑定的报错？

具体显示为： Error in job trial-simplified: SURFACE ASSEMBLY__T0_eularian part-1_M SPECIFIED ON THE *TIE OPTION CONTAINS EULERIAN NODES. NODES ON EULERIAN ELEMENTS CAN NOT BE TIED.

2720 1 3

🍔_6393 3年前

帖子 ABAQUS中隐式和显式的节点和单元的输出变量解析

These variables are set to zero while a secondary node is not in contact. BONDSTAT Field: no History: yes .fil: no Spot weld bond status.

5009 3 2

李时珍 2年前

问答 ABAQUS屈服极限的敏感性分析出错原因？

*Heading** Job name: Job-1 Model name: Model-1** Generated by: Abaqus/CAE 2021*Preprint, echo=NO, model=NO, history=NO, contact=NO***PARAMETERPLAS=380.

2128 2 3

谢宇宸 4年前

帖子沃尔沃XC90空气动力学CFD网格划分

The sides and the top of the domain are treated with symmetry boundary conditions.4 ResultsThe simulations, done with the different meshes (ICEM CFD/TGrid and Harpoon) show in general a good

2664 2 2

网格大师 2年前

帖子 STAR CCM+案例｜救生艇入水仿真救生艇模型

Create a Boundary for Each Part Surface、 Do Not Create Interfaces From Contacts，点击按钮 Apply创建计算区域选择节点 Regions > Background > Boundaries，指定其下子节点的边界类型，如下表所示

3418 5 6

仿真客 3年前

问答

surface timestep = 3.267E-08 controlling slave node ID = 19496138 part ID of slave node = 2 current minimum time step = 3.267E-08 The

3043 1

明月照我程 2年前

帖子 STAR-CCM+变形功能 | 伴随求解优化双元机翼外形

Expand the Regions > Fluid Domain > Boundaries node and select Wing End Plate, Wing Lower Element, and Wing Upper Element.

3749

仿真客 3年前

帖子 abaqus中做的组合结构施加位移荷载的模型，总是出现错误怎么解决

***WARNING: In step 1, portions of main surfaces in the general contact domain have been tied together.

2597 1 1

Coincidence_0550 3年前

帖子 DEP MeshWorks 2021强势发布！

This function is very useful in CFD modeling, where if a user needs to make some closed compartments, by using this function they can get to know how many closed volumes are there in the model.

2312 1 2

DEP MeshWorks 3年前

帖子汽车前沿技术 | NVH前沿工程技术

Predicting acoustic noise and vibration generated by electric machines is challenging due to the variety of physical domains and complex interactions among these domains.

3850 3

声学工程师小吴 2年前

帖子 STAR-CCM+ | 进口控制阀网格划分

Close；重命名 Regions > Subtract节点为 control_valve；展开 Regions > control_valve > Boundaries节点，并设置属性如下： Node

4670 1

乘风破浪_ 2年前

问答 Lsdyna出现“Initialization completed”后就没有了，没有error没有termination

surface timestep = 3.267E-08 controlling slave node ID = 19496138 part ID of slave node = 2 current minimum time step = 3.267E-08 The

2674 2

明月照我程 2年前

帖子 ABAQUS 销轴连接示例

1、进入Step模块，从主菜单中选择Step→Create，命名这个分析步为Contact，接受默认的Static, General，点击Continue。在出现的Edit Step对话框中，接受所有默认选择，并点击OK，创建一个分析步。

3280 2 7

技术为邻 4年前

帖子 Blazek版非结构网格CFD求解器案例分析03：

&e) { Error::Message(e.what()); } // print some statistics cout << " No. of interior nodes: " << solver.geometry.nndInt << endl; cout << " No. of dummy nodes : " << solver.geometry.nNodes

2350 3

网格大师 2年前

帖子 STAR-CCM+ 案例：体积力螺旋桨法

（9）设置边界条件；流体域的边界条件设置类型如下：在Regions > Domain > Boundaries > Aft节点，属性设置如下：同时选择Forward, Port和Starboard，属性设置如下：出口的边界条件设置如下：（10）由于本案例是瞬态模拟，因此需要设置时间步、各时间步内允许的最大内部迭代次数以及获得求解所用的总体物理时间

3512

aero-engine 2年前

帖子 STAR-CCM+怎么画网格？ | 进口控制阀网格划分

Close；重命名 Regions > Subtract节点为 control_valve；展开 Regions > control_valve > Boundaries节点，并设置属性如下： Node

3606 1

仿真客 3年前

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